Regulated three-engined power plant for a rotary wing aircraft

Patent metadata

Field	Value
Publication number	US-9586691-B2
Application number	US-201414333765-A
Country	US
Kind code	B2
Filing date	Jul 17, 2014
Priority date	Jul 23, 2013
Publication date	Mar 7, 2017
Grant date	Mar 7, 2017

Abstract

A power plant ( 1 ) having two engine groups ( 10, 20 ) and a main gearbox (MGB) ( 2 ), and a rotary wing aircraft ( 30 ) having such a power plant ( 1 ). Each engine group ( 10, 20 ) drives said MGB ( 2 ) mechanically to rotate a main outlet shaft ( 3 ) and, consequently, a main rotor ( 31 ) of said aircraft ( 30 ) at a frequency of rotation NR. A first engine group ( 10 ) has two main engines ( 11, 12 ) and is by a first setpoint NR* for said frequency of rotation NR, while a second engine group ( 20 ) has one secondary engine ( 21 ) and is regulated by a second setpoint W 1 * for power from said second engine group ( 20 ). The first engine group ( 10 ) is also regulated by a third setpoint W 2 f* for anticipating power such that said first engine group ( 10 ) and said second engine group ( 20 ) deliver the power needed at said main rotor ( 31 ).

First claim

What is claimed is:

1. A power plant comprising two engine groups and a main gearbox (MGB), the two engine groups driving the MGB mechanically in order to rotate a main outlet shaft of the MGB, the main outlet shaft having a frequency of rotation NR, wherein a first engine group comprises at least one main engine and a first regulator device, the first regulator device regulating operation of each main engine in application of a first setpoint NR* for the frequency of rotation NR of the main outlet shaft, and in that a second engine group comprises at least one secondary engine and a second regulator device, the second regulator device regulating power delivered by each secondary engine in application of a second setpoint W 1 * for the power to be delivered from the second engine group, the power plant having a third regulator device regulating operation of the first engine group in application of a third setpoint W 2 f* for anticipating power to be delivered by the first engine group such that the first engine group and the second engine group together provide a necessary power Ws* needed at the main outlet shaft.

2. The power plant according to claim 1 , wherein the second regulator device includes at least one filter.

3. The power plant according to claim 2 , wherein the third setpoint W 2 f* for anticipating power is such that W 2 f*=W 2 *+H·(W 1 *−W 1 ), (W 1 *−W 1 ) being a difference between the power W 1 , actually delivered by the second engine group and the second setpoint W 1 *, and where H·(W 1 *−W 1 ) is a difference filtered by the at least one filter.

4. The power plant according to claim 1 , wherein the first engine group comprises two identical main engines.

5. The power plant according to claim 1 , wherein the second setpoint W 1 * for power is determined so as to optimize specific consumption of each engine of each of the engine groups.

6. The power plant according to claim 1 , wherein the second setpoint W 1 * for power is determined in order to optimize maintenance of each engine of each of the engine groups.

7. The power plant according to claim 1 , wherein the second setpoint W 1 * for power is determined so as to optimize performance of each engine of each of the engine groups if at least one of the engines fails.

8. The power plant according to claim 1 , wherein the first regulator device includes at least one main computer, each main computer being connected to a single main engine, and the second regulator device includes at least one secondary computer, each secondary computer being connected to a single secondary engine.

9. The power plant according to claim 1 , wherein each secondary engine is a turboshaft engine provided having a gas generator, and the second setpoint W 1 * for power is transformed into a fifth setpoint N 1 * for the frequency of rotation of the gas generator, the second regulator device being configured to transform the second setpoint W 1 * for power into the fifth setpoint N 1 * for frequency of rotation of the gas generator.

10. The power plant according to claim 1 , wherein the at least one main engine of the first engine group is two main engines and the at least one secondary engine of the second engine group is one secondary engine.

11. A power plant comprising two engine groups and a main gearbox (MGB) and a calculator for determining a necessary power Ws* needed at a main outlet shaft of the MGB, the two engine groups driving the MGB mechanically in order to rotate the main outlet shaft of the MGB, the main outlet shaft having a frequency of rotation NR, wherein a first engine group comprises at least one main engine and a first regulator device, the first regulator device regulating operation of each main engine in application of a first setpoint NR* for the frequency of rotation NR of the main outlet shaft, and in that a second engine group comprises at least one secondary engine and a second regulator device, the second regulator device regulating power delivered by each secondary engine in application of a second setpoint W 1 * for the power to be delivered from the second engine group, the power plant having a third regulator device regulating operation of the first engine group in application of a third setpoint W 2 f* for anticipating power to be delivered by the first engine group such that the first engine group and the second engine group together provide the necessary power Ws* needed at the main outlet shaft, wherein the calculator for determining the necessary power Ws* needed at the main outlet shaft of the MGB is configured to determine the necessary power Ws* needed at the main outlet shaft by anticipation of needs for torque and/or power at the main outlet shaft.

12. A method of regulating a power plant for a rotary wing aircraft, the power plant comprising a first engine group, a second engine group, and a main gearbox (MGB), the first and second engine groups driving the MGB mechanically in order to rotate a main outlet shaft of the MGB, the main outlet shaft having a frequency of rotation NR and being constrained to rotate with a main rotor of the aircraft, the method comprising the following steps:
determining a necessary power Ws* needed at the main outlet shaft and a first setpoint NR* for the frequency of rotation NR of the main outlet shaft;
determining a second setpoint W 1 * for power to be delivered by the second engine group;
regulating the first engine group having at least one main engine in application of the first setpoint NR* for the frequency of rotation NR;
regulating the power delivered by the second engine group having at least one secondary engine in application of the second setpoint W 1 * for power;
determining a third setpoint W 2 f* for anticipating power to be delivered by the first engine group; and
regulating the operation of the first engine group in application of the third setpoint W 2 f* for anticipated power such that the first engine group and the second engine group together deliver the necessary power Ws*.

13. The method according to claim 12 for regulating a power plant, wherein power W 1 actually delivered by the second engine group is filtered by at least one filter, the third setpoint W 2 f* for anticipating power being such that W 2 f*=W 2 *+H·(W 1 *−W 1 ), where (W 1 *−W 1 ) being a difference between the power W 1 actually delivered by the second engine group and the second setpoint W 1 * and where H·(W 1 *−W 1 ) is a difference filtered by at least one filter.

Assignees

• Airbus Helicopters

Inventors

• Rossotto Regis
• Boie Hanno

Classifications

• B64D35/08

  characterised by the transmission being driven by a plurality of power plants (for hybrid-electric power plants B64D35/022) · CPC title

• B64D31/09

  in response to power plant failure · CPC title

• B64C27/12 Primary

  Rotor drives · CPC title

• B64C27/00

  Rotorcraft; Rotors peculiar thereto · CPC title

• F05D2270/05

  to affect the output of the engine · CPC title